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Artykuły w czasopismach na temat "Rotor-blade system"
Ngui, Wai Keng, M. Salman Leong, L. M. Hee i Ahmed M. Abdelrhman. "Detection of Twisted Blade in Multi Stage Rotor System". Applied Mechanics and Materials 773-774 (lipiec 2015): 144–48. http://dx.doi.org/10.4028/www.scientific.net/amm.773-774.144.
Pełny tekst źródłaDalli, Uğbreve;ur, i Şcedilefaatdin Yüksel. "Identification of Flap Motion Parameters for Vibration Reduction in Helicopter Rotors with Multiple Active Trailing Edge Flaps". Shock and Vibration 18, nr 5 (2011): 727–45. http://dx.doi.org/10.1155/2011/675791.
Pełny tekst źródłaLee, Yu-Tai, i JinZhang Feng. "Potential and Viscous Interactions for a Multi-Blade-Row Compressor". Journal of Turbomachinery 126, nr 4 (1.10.2004): 464–72. http://dx.doi.org/10.1115/1.1740778.
Pełny tekst źródłaLu, Zhenyong, Shun Zhong, Huizheng Chen, Yushu Chen, Jiajie Han i Chao Wang. "Modeling and Dynamic Characteristics Analysis of Blade-Disk Dual-Rotor System". Complexity 2020 (25.01.2020): 1–13. http://dx.doi.org/10.1155/2020/2493169.
Pełny tekst źródłaWang, Nanfei, Chao Liu i Dongxiang Jiang. "Prediction of transient vibration response of dual-rotor-blade-casing system with blade off". Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, nr 14 (4.04.2019): 5164–76. http://dx.doi.org/10.1177/0954410019839884.
Pełny tekst źródłaLu, Xin, Jie Tang i Liwen Wang. "Simulation and Experimental Study on Rotor System Dynamic Analysis with the Blade-Coating Rubbing Faults". Shock and Vibration 2021 (10.09.2021): 1–15. http://dx.doi.org/10.1155/2021/2442760.
Pełny tekst źródłaZalkind, Daniel S., Gavin K. Ananda, Mayank Chetan, Dana P. Martin, Christopher J. Bay, Kathryn E. Johnson, Eric Loth, D. Todd Griffith, Michael S. Selig i Lucy Y. Pao. "System-level design studies for large rotors". Wind Energy Science 4, nr 4 (11.11.2019): 595–618. http://dx.doi.org/10.5194/wes-4-595-2019.
Pełny tekst źródłaChristensen, René H., i Ilmar F. Santos. "Active Rotor-Blade Vibration Control Using Shaft-Based Electromagnetic Actuation". Journal of Engineering for Gas Turbines and Power 128, nr 3 (1.03.2004): 644–52. http://dx.doi.org/10.1115/1.2056533.
Pełny tekst źródłaAbdelrhman, Ahmed M., M. Salman Leong, Yasin M. Hamdan i Kar Hoou Hui. "Time Frequency Analysis for Blade Rub Detection in Multi Stage Rotor System". Applied Mechanics and Materials 773-774 (lipiec 2015): 95–99. http://dx.doi.org/10.4028/www.scientific.net/amm.773-774.95.
Pełny tekst źródłaQian, Xiaoru, Peigang Yan, Xiangfeng Wang i Wanjin Han. "Numerical Analysis of Conjugated Heat Transfer and Thermal Stress Distributions in a High-Temperature Ni-Based Superalloy Turbine Rotor Blade". Energies 15, nr 14 (7.07.2022): 4972. http://dx.doi.org/10.3390/en15144972.
Pełny tekst źródłaRozprawy doktorskie na temat "Rotor-blade system"
Pickering, Todd Michael. "Methods for Validation of a Turbomachinery Rotor Blade Tip Timing System". Thesis, Virginia Tech, 2014. http://hdl.handle.net/10919/47496.
Pełny tekst źródłaMaster of Science
Prechtl, Eric Frederick. "Design and implementation of a piezoelectric servo-flap actuation system for helicopter rotor individual blade control". Thesis, Massachusetts Institute of Technology, 2000. http://hdl.handle.net/1721.1/9266.
Pełny tekst źródłaIncludes bibliographical references (p. 177-186).
A novel new actuator for helicopter rotor control, the X-Frame Actuator, was developed, demonstrating superior performance for applications requiring compact, fast acting, large stroke actuation. The detailed experimental characterization of this actuator is described, including bench-top output energy measurements and transverse shake test performance. A Mach scaled rotor blade utilizing the X-Frame actuator to power a trailing edge servo-flap near the tip was also designed, manufactured and tested. A description of the design and composite manufacturing of the rotor blade and servo-flap is presented. Preliminary bench tests of the active blade actuation system are also presented. The hover tests of the active blade provided transfer function identification of the performance of the actuator in producing flap deflections, and the response of the rotor from deflections of the servo-flap. At the highest field level of 60 V/mil P-P the actuation system produces 7.75 degrees of quasi-static peak-to-peak flap deflection in hover. The servo-flap produces significant control authority, especially near the 3/rev frequency that would be important for the CH-47. Scaled to a full-sized CH-47, the rotor can produce over 16,000 lb peak-to-peak thrust variation at 3/rev, which is 32% of the aircraft's gross weight. Closed-loop feedback control was experimentally applied to the model rotor system. Both single frequency and combined frequency controllers were successfully implemented on the rotor. Most significantly, simultaneous control of 1/rev, 3/rev, 4/rev, 5/rev, and 6/rev harmonic vibration has been successfully demonstrated. The peak vibrations were eliminated at each frequency, as well as the vibrations over a small bandwidth surrounding each peak. Experimental comparison of continuous time versus discrete time control has shown the former to be a more effective approach for vibration reduction.
by Eric Blade Prechtl.
Ph.D.
Roth, Brian D. "Acoustic source and data acquisition system for a helicopter rotor blade-vortex interaction (BVI) noise reduction experiment". Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1996. http://handle.dtic.mil/100.2/ADA326229.
Pełny tekst źródła"December 1996." Thesis advisor(s): Robert M. Keolian, Steven R. Baker. Includes bibliographical references (p. 59). Also available online.
Mansisidor, Michael R. "Resonant blade response in turbine rotor spin tests using a laser-light probe non-intrusive measurement system". Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2002. http://sirsi.nps.navy.mil/uhtbin/hyperion-image/j02Mar%5FMansisidor.pdf.
Pełny tekst źródłaSánchez, Jiménez Oscar. "On the stochastic response of rotor-blade models with Floquet modal theory : applications to time-dependent reliability of tidal turbine blades". Electronic Thesis or Diss., Normandie, 2023. http://www.theses.fr/2023NORMIR39.
Pełny tekst źródłaThe response of a deterministic rotating mechanical system under stochastic excitation is studied. A mechanical-probabilistic model is developed to combine the relevant characteristics of both aspects of the study: the behavior of this non-standard class of mechanical system and the random properties of correlated stochastic fields describing load processes. The results are applied to a reliability analysis of a reduced order model of a tidal turbine. Semi-analytic and empirical ( in the Monte-Carlo simulation sense) results are obtained, compared and contrasted. The results are framed with respect to the existing literature, and it is found that they provide an innovative treatment of the problem, in terms of the dynamical choices reflected in the model, in the presentation and interpretation of the modal aspects of the system, and in the type of stochastic inputs considered. We develop a dynamical model describing a broad class of mechanical system that models a rotor-blade structure. The model is informed by careful consideration of previous results, with the aim of constructing a reduced model that captures essential characteristics of the vibratory behavior of the structure. Lagrangian formalism is utilized to obtain the equations of motion. The presence of elastic components, which are discretized in a modal way, results in a system of ordinary differential equations with periodic coefficients. The Floquet theory of Linear time-periodic systems is applied on the deterministic dynamical model to synthesize an extension of traditional modal analysis to systems with periodic coefficients. The response of the system is formulated in terms of Floquet exponents and the associated Floquet periodic eigenvectors, from which the Floquet State Transition Matrix can be obtained. Several methods are applied to the modal study of the system, and a new time-frequency approach is proposed based on PGHW wavelets and its associated scalogram. Using an innovative notation to describe probabilistic moments of stochastic quantities, a moment propagation scheme is presented and exploited. The advantages of the treatment, particularly in the case of spatio-temporal stochastic fields, is in its applicability and systematic structure of development. This moment propagation strategy is coupled with a maximum entropy formulation to reconstruct the probability density function of the response and obtain important descriptors of the response, such as the Extreme Value Distribution. The moment propagation technique presented is applied to nonstationary processes. The results from Modal Floquet theory are integrated into this analysis. The problem of crossings of a certain threshold is considered for this type of nonstationary stochastic process. Their response is shown to yield a time-dependent reliability problem, which is resolved using the estimated EVD and then by numerical simulation
Pawar, Prashant M. "Structural Health Monitoring Of Composite Helicopter Rotor Blades". Thesis, Indian Institute of Science, 2006. http://hdl.handle.net/2005/273.
Pełny tekst źródłaPawar, Prashant M. "Structural Health Monitoring Of Composite Helicopter Rotor Blades". Thesis, Indian Institute of Science, 2006. https://etd.iisc.ac.in/handle/2005/273.
Pełny tekst źródłaDen, Heijer Francois Malan. "Development of an active pitch control system for wind turbines / F.M. den Heijer". Thesis, North-West University, 2008. http://hdl.handle.net/10394/2635.
Pełny tekst źródłaThesis (M.Ing. (Mechanical Engineering))--North-West University, Potchefstroom Campus, 2009.
Fowler, Leslie Paige. "Application of the Filtered-X LMS Algorithm for Disturbance Rejection in Time-Periodic Systems". Thesis, Virginia Tech, 1996. http://hdl.handle.net/10919/36768.
Pełny tekst źródłaMaster of Science
Griffith, Khadir A. "Performance Evaluation of RF Systems on Rotorcrafts". The Ohio State University, 2010. http://rave.ohiolink.edu/etdc/view?acc_num=osu1274103965.
Pełny tekst źródłaKsiążki na temat "Rotor-blade system"
Y, Chu Alphonse, Talbot Peter D i United States. National Aeronautics and Space Administration., red. Synthesis of individual rotor blade control system for gust alleviation: Final report. [Washington, D.C: National Aeronautics and Space Administration, 1990.
Znajdź pełny tekst źródłaAcoustic source and data acquisition system for a helicopter rotor blade-vortex interaction (BVI) noise reduction experiment. Monterey, Calif: Naval Postgraduate School, 1996.
Znajdź pełny tekst źródłaH, Mirick Paul, Langston Chester W i Langley Research Center, red. Rotating shake test and modal analysis of a model helicopter rotor blade. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
Znajdź pełny tekst źródłaM, Bartie K., i Ames Research Center, red. Hover performance tests of baseline metal and Advanced Technology Blade (ATB) rotor systems for the XV-15 tilt rotor aircraft. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.
Znajdź pełny tekst źródłaNational Aeronautics and Space Administration (NASA) Staff. Synthesis of Individual Rotor Blade Control System for Gust Alleviation. Independently Published, 2018.
Znajdź pełny tekst źródłaAcoustic Source and Data Acquisition System for a Helicopter Rotor Blade-Vortex Interaction (BVI) Noise Reduction Experiment. Storming Media, 1996.
Znajdź pełny tekst źródłaResonant Blade Response in Turbine Rotor Spin Tests Using a Laser-Light Probe Non-Intrusive Measurement System. Storming Media, 2002.
Znajdź pełny tekst źródłaNational Aeronautics and Space Administration i NASA. Preliminary Design Study of Advanced Composite Blade and Hub and Nonmechanical Control System for the Tilt-Rotor Aircraft - Volume 2 : Project Planning Data: February 1 1980. Independently Published, 2022.
Znajdź pełny tekst źródłaCzęści książek na temat "Rotor-blade system"
Ma, Hui, Zhiyuan Wu, Xingyu Tai, Chaofeng Li i Bangchun Wen. "Nonlinear Behavior Analysis Caused by Blade Tip Rubbing in a Rotor-Disk-Blade System". W Proceedings of the 9th IFToMM International Conference on Rotor Dynamics, 181–91. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-06590-8_15.
Pełny tekst źródłaZhang, Jian, Shiping Song, Chao Li, Yanhong Ma i Jie Hong. "Dynamic Analysis and Safety Design for Aero-Engine Rotor-Support System Under the Blade-off". W Proceedings of the 11th IFToMM International Conference on Rotordynamics, 1–14. Cham: Springer International Publishing, 2023. http://dx.doi.org/10.1007/978-3-031-40455-9_1.
Pełny tekst źródłaLin, Jiewei, Bin Wu, Xin Lu, Jian Xu, Junhong Zhang i Huwei Dai. "Numerical Simulation of Aero-Engine Rotor-Blade-coating Coupling System with Rub-impact Fault and Its Dynamic Response". W Proceedings of the 11th IFToMM International Conference on Rotordynamics, 56–75. Cham: Springer International Publishing, 2023. http://dx.doi.org/10.1007/978-3-031-40459-7_4.
Pełny tekst źródłaMa, Yanhong, Yongfeng Wang i Jie Hong. "Dynamic Model and Theoretical Investigation for the Fan-Blade Out Event in the Flexible Rotor System of Aero-Engine". W Mechanisms and Machine Science, 18–33. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-99272-3_2.
Pełny tekst źródłaLuthfi, Muhammad, Leo Van Gunawan, Muhamad Ghozali, Reza Aditya i Saeful Anwar. "Experimental Study of Multistage Rotor in Gravitational Water Vortex Turbine System with Various Gap Placement Positions and Blade Phase-Shift Angles". W Proceedings of the International Conference on Applied Science and Technology on Engineering Science 2023 (iCAST-ES 2023), 992–1000. Dordrecht: Atlantis Press International BV, 2024. http://dx.doi.org/10.2991/978-94-6463-364-1_91.
Pełny tekst źródłaSoodani, Sara, SeyedVahid Hosseini, Mohammad Hakimi i Mohammad Akhlaghi. "The Effect of Vane Number in Casing Treatment of an Axial-Flow Compressor". W Springer Proceedings in Energy, 341–50. Cham: Springer Nature Switzerland, 2023. http://dx.doi.org/10.1007/978-3-031-30960-1_32.
Pełny tekst źródłaSchleupen, Josef, Heiko Engemann, Mohsen Bagheri, Stephan Kallweit i Peter Dahmann. "Developing a Climbing Maintenance Robot for Tower and Rotor Blade Service of Wind Turbines". W Advances in Intelligent Systems and Computing, 310–19. Cham: Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-49058-8_34.
Pełny tekst źródłaMaraev, Anton A., Gennady A. Shut, Alexander N. Timofeev, Sergey V. Mikheev, Artem Kh Akhmerov, Liliana S. Rodikova i Igor A. Konyakhin. "Effect of Illumination on Errors in Estimation of a Rotor Blade Chord Value During Intelligent Video Endoscopy of a Closed Steam Turbine Cylinder". W Studies in Systems, Decision and Control, 169–85. Cham: Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-030-97004-8_13.
Pełny tekst źródłaSun, Fengnan, Yan Zhu, Qiyou Cheng, Siwen Wang i Longtao Xing. "Simulation and Analysis of Dynamic Characteristics of Tilt Rotor/Wing Coupling System". W Advances in Transdisciplinary Engineering. IOS Press, 2022. http://dx.doi.org/10.3233/atde221044.
Pełny tekst źródłaNikolaev, Evgeny, i Maria Nikolaeva. "Discrete Vortex Cylinders Method for Calculating the Helicopter Rotor-Induced Velocity". W Vortex Dynamics Theories and Applications. IntechOpen, 2020. http://dx.doi.org/10.5772/intechopen.93186.
Pełny tekst źródłaStreszczenia konferencji na temat "Rotor-blade system"
Yi, Liu. "Dynamic analysis of rotor blade system". W 2017 19th International Conference on Advanced Communication Technology (ICACT). IEEE, 2017. http://dx.doi.org/10.23919/icact.2017.7890250.
Pełny tekst źródłaJones, Henry. "A Nonintrusive Rotor Blade Vibration Monitoring System". W ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1996. http://dx.doi.org/10.1115/96-gt-084.
Pełny tekst źródłaYi, Liu. "The dynamical model of rotor blade system". W 2016 18th International Conference on Advanced Communication Technology (ICACT). IEEE, 2016. http://dx.doi.org/10.1109/icact.2016.7423381.
Pełny tekst źródłaYi, Liu. "The dynamical model of rotor blade system". W 2016 18th International Conference on Advanced Communication Technology (ICACT). IEEE, 2016. http://dx.doi.org/10.1109/icact.2016.7423382.
Pełny tekst źródłaAl-Nassar, Y. N. "Finite Element Modeling of Blade-Rotor System in Turbomachinery". W ASME 2003 Pressure Vessels and Piping Conference. ASMEDC, 2003. http://dx.doi.org/10.1115/pvp2003-2179.
Pełny tekst źródłaAdewusi, Surajudeen. "Detection of Rotating Blade Faults From Lateral Vibrations of a Rotor-Disk-Blade System". W ASME 2015 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/detc2015-46567.
Pełny tekst źródłaSimmons, Harold R., Douglas L. Michalsky, Kenneth E. Brewer i Anthony J. Smalley. "Measuring Rotor and Blade Dynamics Using an Optical Blade Tip Sensor". W ASME 1990 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1990. http://dx.doi.org/10.1115/90-gt-091.
Pełny tekst źródłaKarlsson, B. Agne, C. Pontus Bergström i J. Thomas F. Domeij. "Rotor Dynamic Response at Blade Loss". W ASME 1999 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1999. http://dx.doi.org/10.1115/99-gt-201.
Pełny tekst źródłaMileshin, Victor, Victor Fateev i Alexander Stepanov. "Blade Fissure Determination by Means of Blade Tip-Timing System". W ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/gt2018-76848.
Pełny tekst źródłaOkabe, Akira, Takeshi Kudo, Hideo Yoda, Shigeo Sakurai, Osami Matsushita i Koki Shiohata. "Rotor-Blade Coupled Vibration Analysis by Measuring Modal Parameters of Actual Rotor". W ASME Turbo Expo 2009: Power for Land, Sea, and Air. ASMEDC, 2009. http://dx.doi.org/10.1115/gt2009-59471.
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